ES2719437T3 - Dispositivo de asistencia de un sistema propulsor de propergol sólido de un helicóptero monomotor, helicóptero monomotor que comprende dicho dispositivo - Google Patents

Dispositivo de asistencia de un sistema propulsor de propergol sólido de un helicóptero monomotor, helicóptero monomotor que comprende dicho dispositivo Download PDF

Info

Publication number
ES2719437T3
ES2719437T3 ES15719802T ES15719802T ES2719437T3 ES 2719437 T3 ES2719437 T3 ES 2719437T3 ES 15719802 T ES15719802 T ES 15719802T ES 15719802 T ES15719802 T ES 15719802T ES 2719437 T3 ES2719437 T3 ES 2719437T3
Authority
ES
Spain
Prior art keywords
turbine
power transmission
power
transmission box
helicopter
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
ES15719802T
Other languages
English (en)
Spanish (es)
Inventor
Romain Thiriet
Camel Serghine
Patrick Marconi
Jean-Louis Besse
Pascal Guillemet
Guillaume Demezon
Philippe Barrat
François Danguy
Jean-Michel Sannino
De Chanaud Nicolas Marucheau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Safran Helicopter Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Safran Helicopter Engines SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS, Safran Helicopter Engines SAS filed Critical Safran Aircraft Engines SAS
Application granted granted Critical
Publication of ES2719437T3 publication Critical patent/ES2719437T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/006—Safety devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • F02C7/277—Mechanical drives the starter being a separate turbine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/092—Purpose of the control system to cope with emergencies in particular blow-out and relight
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Eletrric Generators (AREA)
ES15719802T 2014-04-08 2015-04-03 Dispositivo de asistencia de un sistema propulsor de propergol sólido de un helicóptero monomotor, helicóptero monomotor que comprende dicho dispositivo Active ES2719437T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1453123A FR3019588B1 (fr) 2014-04-08 2014-04-08 Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif et procede correspondant
PCT/FR2015/050878 WO2015155450A1 (fr) 2014-04-08 2015-04-03 Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif

Publications (1)

Publication Number Publication Date
ES2719437T3 true ES2719437T3 (es) 2019-07-10

Family

ID=51483532

Family Applications (1)

Application Number Title Priority Date Filing Date
ES15719802T Active ES2719437T3 (es) 2014-04-08 2015-04-03 Dispositivo de asistencia de un sistema propulsor de propergol sólido de un helicóptero monomotor, helicóptero monomotor que comprende dicho dispositivo

Country Status (10)

Country Link
US (1) US20170114723A1 (enrdf_load_stackoverflow)
EP (1) EP3129619B1 (enrdf_load_stackoverflow)
JP (1) JP6740137B2 (enrdf_load_stackoverflow)
KR (1) KR102258405B1 (enrdf_load_stackoverflow)
CN (1) CN106536350B (enrdf_load_stackoverflow)
CA (1) CA2944839C (enrdf_load_stackoverflow)
ES (1) ES2719437T3 (enrdf_load_stackoverflow)
FR (1) FR3019588B1 (enrdf_load_stackoverflow)
RU (1) RU2684693C2 (enrdf_load_stackoverflow)
WO (1) WO2015155450A1 (enrdf_load_stackoverflow)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3019524B1 (fr) * 2014-04-03 2017-12-08 Turbomeca Chaine motrice pour helicoptere incorporant un module moteur pyrotechnique d'assistance et helicoptere la comportant
IL242061B (en) * 2015-10-13 2020-05-31 Newrocket Ltd Thrusting rockets
FR3050765B1 (fr) * 2016-04-28 2018-04-27 Safran Helicopter Engines Systeme auxiliaire d'entrainement d'un arbre d'un systeme propulsif d'un helicoptere
FR3050815B1 (fr) * 2016-04-28 2019-05-24 Safran Helicopter Engines Systeme d'allumage et dispositif d'entrainement mecanique associe
FR3062882B1 (fr) 2017-02-15 2019-10-18 Safran Helicopter Engines Systeme propulsif d'un helicoptere monomoteur
FR3062881B1 (fr) 2017-02-15 2019-03-15 Safran Helicopter Engines Procede et systeme de commande d'un dispositif d'urgence
US11001384B2 (en) * 2017-10-02 2021-05-11 Bell Helicopter Textron Inc. Hybrid power systems for aircraft
FR3081150B1 (fr) * 2018-05-18 2020-06-12 Safran Helicopter Engines Architecture de puissance d'un aeronef
FR3104136A1 (fr) * 2019-12-10 2021-06-11 Airbus Operations (S.A.S.) Système de propulsion d’un aéronef
FR3104333A1 (fr) * 2019-12-10 2021-06-11 Airbus Operations (S.A.S.) Aéronef comprenant une source de secours d’énergie électrique.
FR3117450B1 (fr) 2020-12-11 2024-03-01 Safran Helicopter Engines Système propulsif hybride pour un hélicoptère
US11794914B2 (en) 2021-07-19 2023-10-24 Pratt & Whitney Canada Corp. Emergency power unit for electric aircraft

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB605971A (en) * 1944-12-30 1948-08-04 British Thomson Houston Co Ltd Improvements relating to speed governors for rotary wing aircraft
US2460246A (en) * 1945-04-07 1949-01-25 Redmond Company Inc Speed-responsive rheostat
US2986879A (en) * 1957-06-12 1961-06-06 Bendix Corp Solid propellant starter
GB1389403A (en) * 1971-06-01 1975-04-03 Westland Aircraft Ltd Helicopter power transmission systems
US5020316A (en) * 1989-05-19 1991-06-04 Coltec Industries Inc. Helicopter control with multiple schedule rotor speed decay anticipator
JPH05193579A (ja) * 1992-01-20 1993-08-03 Mitsubishi Heavy Ind Ltd ターボシャフト・エンジン
RU2065381C1 (ru) * 1993-01-19 1996-08-20 Вертолетный научно-технический комплекс им.Н.И.Камова Главный редуктор вертолета
US7032860B1 (en) * 2004-11-05 2006-04-25 Eatts, Llc Emergency anti-torque thruster system
FR2922860B1 (fr) * 2007-10-26 2010-01-22 Eurocopter France Amelioration aux giravions equipes de turbomoteurs
GB2460246B (en) * 2008-05-21 2012-09-19 Matthew P Wood Helicopter with auxiliary power unit for emergency rotor power
FR2967132B1 (fr) * 2010-11-04 2012-11-09 Turbomeca Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre
FR2990004B1 (fr) 2012-04-27 2014-04-18 Turbomeca Procede et systeme de demarrage d'urgence d'architecture generatrice d'energie
FR2992024B1 (fr) * 2012-06-15 2017-07-21 Turbomeca Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere

Also Published As

Publication number Publication date
FR3019588A1 (fr) 2015-10-09
JP6740137B2 (ja) 2020-08-12
CN106536350A (zh) 2017-03-22
RU2016142637A3 (enrdf_load_stackoverflow) 2018-10-29
KR20170002400A (ko) 2017-01-06
EP3129619B1 (fr) 2019-02-27
CN106536350B (zh) 2021-10-19
JP2017521589A (ja) 2017-08-03
FR3019588B1 (fr) 2019-06-14
WO2015155450A1 (fr) 2015-10-15
RU2684693C2 (ru) 2019-04-11
EP3129619A1 (fr) 2017-02-15
US20170114723A1 (en) 2017-04-27
CA2944839A1 (fr) 2015-10-15
KR102258405B1 (ko) 2021-05-31
RU2016142637A (ru) 2018-05-08
CA2944839C (fr) 2022-11-01

Similar Documents

Publication Publication Date Title
ES2719437T3 (es) Dispositivo de asistencia de un sistema propulsor de propergol sólido de un helicóptero monomotor, helicóptero monomotor que comprende dicho dispositivo
CN113302130B (zh) 返回基地的太空运载火箭系统和方法
TWI686327B (zh) 多旋翼飛行器
US11149633B2 (en) System of using compressed air as a force source and method thereof; airplane
JP2017521589A5 (enrdf_load_stackoverflow)
US11821360B2 (en) Aircraft propulsion system and aircraft powered by such a propulsion system built into the rear of an aircraft fuselage
ES2649552T3 (es) Sistema y procedimiento de arranque de emergencia de una turbomáquina de aeronave
EP3418670B1 (en) Parallel combustor configuration for unmanned underwater vehicle propulsion turbine
CN110312854A (zh) 用于单引擎直升机的推进系统
US20180037319A1 (en) Vertical take-off and landing aircraft (variants)
US12252244B2 (en) Vertical take off and landing flying machine
EP3234499B1 (en) Launcher redundant tank mass shedding system
ES2288083A1 (es) Disposicion sustentadora para aeronaves de despegue y aterrizaje vertical.
US20170015411A1 (en) Drive chain for a helicopter incorporating a pyrotechnic assistance drive module and helicopter comprising the same
ES2367501B1 (es) Sistema sustentador, propulsor y estabilizador para aeronaves de despegue y aterrizaje vertical.
RU2475417C1 (ru) Летательный аппарат "летающая тарелка"
RU2473819C1 (ru) Двигательная установка системы аварийного спасения
RU2471676C1 (ru) Летательный аппарат "летающая тарелка"
RU2710843C1 (ru) Боевой самолет вертикального взлета и посадки
RU2532445C1 (ru) Компоновка многоступенчатой ракеты-носителя
RU2710038C1 (ru) Самолет вертикального взлета и посадки